View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62568U 26145.53684655 +.00000000 +00000-0 +55094-3 0 00006
2 62568 43.0018 218.7280 0001865 271.9579 88.1059 15.27597935 07
| Epoch (UTC): | 25 May 2026 12:53:03 |
| Eccentricity: | 0.0001865 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 218.7280° |
| argument of perigee: | 271.9579° |
| revolutions per day: | 15.27597935 |
| mean anomaly at epoch: | 88.1059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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